EP1778540B1 - Anordnung des oberen teils einer flugzeugkabine - Google Patents

Anordnung des oberen teils einer flugzeugkabine Download PDF

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Publication number
EP1778540B1
EP1778540B1 EP05791092.9A EP05791092A EP1778540B1 EP 1778540 B1 EP1778540 B1 EP 1778540B1 EP 05791092 A EP05791092 A EP 05791092A EP 1778540 B1 EP1778540 B1 EP 1778540B1
Authority
EP
European Patent Office
Prior art keywords
cabin
aisle
fact
seats
bridge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP05791092.9A
Other languages
English (en)
French (fr)
Other versions
EP1778540A1 (de
Inventor
Bruno Saint-Jalmes
André Rezag
Jazon Zaneboni
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus SAS
Original Assignee
Airbus SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from FR0408239A external-priority patent/FR2873349B1/fr
Application filed by Airbus SAS filed Critical Airbus SAS
Publication of EP1778540A1 publication Critical patent/EP1778540A1/de
Application granted granted Critical
Publication of EP1778540B1 publication Critical patent/EP1778540B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0601—Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
    • B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D2011/0069—Rest berths, beds or the like
    • B64D2011/0084—Bed units for passengers attached to the ceiling of the fuselage

Definitions

  • the present invention relates to an arrangement of the upper part of the cabin of an aircraft.
  • the technical field of the invention is the transport of passengers in an aircraft.
  • first class the cabin of an aircraft, it is advisable to have as many passengers as possible by offering them maximum comfort.
  • business class the seats offered to travelers are most often convertible seats that offer in a first position a seating position to the passenger and in another position a recumbent position, more or less inclined in business class.
  • Various solutions are known from the prior art to also provide sleeping places for economy class travelers. For example, it has been proposed to use several seats to convert them into bunk beds. Generally the number of berths obtained is less than the number of seats. In known solutions, there are generally two seats for a berth.
  • the idea behind the present invention is to use the upper space of the cabin of the aircraft to have berths there.
  • the problem is to be able to have a large number of berths.
  • the present invention is then intended to provide a number of berths in the upper space of the cabin of an aircraft.
  • the bunks served by the raised aisle are arranged transversely to the aisle and on both sides thereof.
  • the invention also provides a preferred embodiment in which the bunks are suspended from the side of the central aisle to the main structure of the cabin and are connected on the opposite side to the aisle to the same structure.
  • the elements then supporting the berths can have both a lightweight structure and also be resistant because they are attached to the main structure of the cabin.
  • the berths are supported by L-shaped structural members, a first leg of the L extending substantially parallel to the bridge and having a length substantially equal to the length of a bunk while that the other leg of the L extends substantially perpendicularly to the first leg, and the free ends of the L-shaped structural members are fixed to the main structure of the cabin.
  • the raised aisle is advantageously supported by the deck of the cabin. This is not a significant overload for the cabin deck.
  • the elevated driveway may replace a column of seats and the weight of the elements to make a raised walkway should not be greater than the weight of a column of seats, even if they are seats economy class.
  • staircase provides access to each end of the raised walkway.
  • This staircase can be oriented longitudinally in the cabin, or transversely. In the case of a transversal staircase, this one can be double (access then to the alley by the left and by the right).
  • a curved staircase A ladder could also allow access to the driveway.
  • this solution although conceivable and cheaper than a staircase, is not a priori preferred solution because it does not allow rapid evacuation of passengers out of the berths served by the raised walkway.
  • the raised aisle longitudinally divides the cabin into two longitudinal sections. There is then in such an aircraft a "wall" longitudinally separating the cabin in two. This allows for an aisle with a relatively large height allowing passengers accessing the bunks to walk upright without having to bend.
  • convertible seats berths are for example all in the same longitudinal section.
  • passages for air ducts and pipes are advantageously provided in a structure supporting the deck.
  • storage spaces are arranged under the raised aisle. This allows to have luggage boxes very accessible.
  • a luggage compartment placed on the ground is of lesser weight than a conventional chest arranged in height. As there is a lot of room under the elevated driveway, this place can also be used to store trolleys used by cabin crew to provide passenger service. It can also accommodate elements fixed on the ground, called monuments. It can for example be kitchens used for cabin service (generally called “galleys”) or also wardrobes for receiving jackets and coats passengers (these wardrobes are generally referred to as "coat stowage”) .
  • the deck ceiling is preferably substantially parallel to the deck.
  • first compartment 6 At the front of the cabin 4, there is a first compartment 6 in which are arranged individual modules for passenger 8.
  • each individual passenger module 8 is a convertible seat that can accommodate a passenger in both sitting and lying. Other comfort equipment is also provided in this module.
  • Compartment 6 is here called first class compartment.
  • a second compartment 10 which comprises on the one hand seats 12 (not convertible into a bed) and on the other hand bunks 14.
  • the seats 12 and the berths 14 are arranged at different levels. .
  • the berths 14 are located above seats 12, all the seats 12 being at the same level, corresponding to the level at which the passenger individual modules 8 are located.
  • This second compartment 10 is described in more detail below.
  • a third compartment 16 in which are arranged seats 12 similar to the seats of the second compartment 10. These seats 12 are arranged at the same level as the seats 12 of the second compartment 10 and that the individual modules for passenger 8 of the first compartment 6,
  • the figure 2 corresponds to a sectional view of the fuselage of the aircraft of the figure 1 , the section being made at the second compartment 10.
  • a main structure 18 of the aircraft is shown schematically at the periphery of the cabin by a double line.
  • This may be a conventional aircraft structure as known to those skilled in the art.
  • a bridge 20 extending longitudinally with respect to the aircraft separates the cabin 4 from a cargo hold 22.
  • the deck 20 is supported by a structure 24 formed in particular of beams fixed on the main structure 18.
  • the cargo hold 22 has a floor 26 is is intended to receive, in its part at the cutting plane, standardized containers 28.
  • bridge 20 is horizontal and extends in the same plane over the entire length and width of the aircraft. It is also assumed that the cabin is above the deck while the cargo compartment is below it.
  • the berths 14 In the upper part of the cabin 4, and more precisely the second compartment 10, are the berths 14. The latter are arranged horizontally that is to say parallel to the bridge 20 and are oriented transversely relative to the cabin. As we see in particular on the figure 1 here, there are two rows of bunks 14. These two rows are arranged on either side of a central aisle 32.
  • the berths 14 are supported by L-shaped carrying elements 34. These carrying elements 34 are arranged in such a way that one leg of the L extends horizontally and the other leg extends vertically towards the top of the cabin. 4. The free ends of the branches of the L are each attached to the main structure 18 of the cabin. Two mezzanines extending longitudinally on both sides of the aircraft are thus produced. Lane 32 provides access to these mezzanines. It has a floor 36 comparable to a bridge fixed on the deck 20. A raised road is thus made with respect to the bridge 20 in the center of the cabin 4. Access to this path is via two staircases 38 , a staircase at each end of the aisle 32. A side wall 40 connects on each side of the aisle 32 the ground 36 thereof to the bunks 14. The aisle 32 is thus isolated from the rest of the second compartment 10.
  • the floor 36 preferably rests on storage lockers. These can be used to accommodate the baggage of the passengers of the second compartment 10. There is under the ground 36 enough room to accommodate all the luggage of the passengers traveling in the second compartment if one takes into account the maximum acceptable size of the luggage usually allowed to travel in the cabin. There is even enough room to house under the ground 36 trolleys (galleys) usually used by commercial cabin crew to perform the service on board the aircraft. The presence of this storage space allows to remove in the cabin luggage racks that are usually found in height. In this way, in the upper part of the cabin, more space is available and this place is used for the comfort of the passengers in the berths 14.
  • the structure 24 carrying the bridge 20 is organized to allow the passage of various pipes and conduits.
  • various pipes and conduits For example, electrical bundles, hydraulic lines and pneumatic lines are passed.
  • Air ducts for ventilation of the cabin can take place in the bunkers 22, just under the structure 24 carrying the bridge 20 and close to the outer wall of the aircraft. The location receiving these air ducts is identified by reference 41.
  • These pipes then pass between structural connecting rods and the skin of the aircraft.
  • pipes may be provided along transverse structural elements called frames for supplying air to this part of the cabin 4.
  • the figure 3 shows an alternative embodiment of the figure 2 .
  • the difference is that there are three front seats on each side of the center aisle at deck 20 whereas, as can be seen in the drawing, there are four in the configuration of the figure 2 .
  • the configuration represented on the figure 4 is original in that convertible seats 42 are arranged on one side of the aisle 32 central while on the other side of this aisle there are seats 12 corresponding to the seats that are usually in the compartments of economy class.
  • the seats corresponding to the economy class are arranged at the bottom of the cabin while the first classes and business classes are arranged towards the front of the cabin.
  • the first class and business class passengers are placed on the right side of the aircraft, in relation to the direction of the aircraft's flight (ie left on the figure 4 ) and economy class passengers on the left of the plane.
  • economy class passengers no longer cross first class and business class compartments and are directed directly to the economy class compartment.
  • the proposed solution for making berths does not cause significant overweight for the aircraft. Indeed, as indicated above, the proposed solution leads to the removal of all the luggage boxes placed in height. These chests have a relatively large mass. A very significant weight gain is achieved by replacing these luggage compartments usually arranged in height by lockers placed on the deck and serving as a floor support 36 of the aisle 32 central.
  • the proposed solution provides a driveway 32 in which passengers can move without having to bend. It is thus possible to perform the evacuation of the aircraft within the time prescribed by the aeronautical standards.
  • the berths 14 can thus be arranged at a distance from the deck barely greater than the height of a man.
  • the level of these berths can therefore be substantially lowered compared to prior art berths which are located in the upper part of the cabin of an aircraft. This lowering of the level of the berths allows in particular to benefit from a greater width at the level of the berths and allows to have in the upper part of the cabin, on the same level, two persons lying transversely to the direction of the march of the aircraft as well as a central aisle.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Claims (9)

  1. Flugzeugkabine (4), die für die Beförderung von Passagieren bestimmt ist, umfassend:
    - eine Hauptstruktur (18), die der Struktur des Flugzeugs entspricht und die Kabine (4) umgibt,
    - eine Brücke (20), die eine ebene Fläche bildet, auf der Sitze (12, 42) befestigt sind,
    - einen Gang (32), der sich längs in der Kabine (4) erstreckt und in Bezug zur Brücke (20) erhöht ist, und
    - Kojen (14), die vom Gang (32) aus zugänglich sind und über Sitzen (12, 42) der Brücke (20) angeordnet sind,
    dadurch gekennzeichnet, dass
    - der Längsgang (32) ein Mittelgang ist,
    - die Kojen (14), die vom erhöhten Gang (32) aus zugänglich sind, quer zum Gang (32) und auf beiden Seiten desselben angeordnet sind, und
    - die Kojen (14) auf der Seite des Mittelgangs (32) an der Hauptstruktur (18) der Kabine (4) aufgehängt und auf der dem Gang gegenüberliegenden Seite mit derselben Struktur (18) verbunden sind.
  2. Flugzeugkabine (4) nach Anspruch 1, dadurch gekennzeichnet, dass die Kojen (14) von L-förmigen Strukturelementen (34) getragen werden, wobei sich ein erster Schenkel des L im Wesentlichen parallel zur Brücke (20) erstreckt und eine Länge im Wesentlichen gleich der Länge einer Koje (14) aufweist, während sich der andere Schenkel des L im Wesentlichen senkrecht auf den ersten Schenkel erstreckt, und dass die freien Enden der L-förmigen Strukturelemente (34) an der Hauptstruktur (18) der Kabine (4) befestigt sind.
  3. Flugzeugkabine (4) nach einem der Ansprüche 1 und 2, dadurch gekennzeichnet, dass der erhöhte Gang (32) von der Brücke (20) der Kabine getragen wird.
  4. Flugzeugkabine (4) nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass es eine Treppe (38) ermöglicht, Zugang zu jedem der Enden des erhöhten Gangs (32) zu erhalten.
  5. Flugzeugkabine (4) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass der erhöhte Gang (32) die Kabine (4) längs in zwei Längsabschnitte teilt.
  6. Flugzeugkabine (4) nach Anspruch 5, dadurch gekennzeichnet, dass die Kabine (4) zu Kojen verwandelbare Sitze (42) und nicht zu Kojen verwandelbare Sitze (12) aufweist, und dass die zu Kojen verwandelbaren Sitze (42) alle in einem selben Längsabschnitt angeordnet sind.
  7. Flugzeugkabine (4) nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass Durchgänge für Luftleitungen und Kanalisationen in einer Struktur (24), die die Brücke (20) trägt, vorgesehen sind.
  8. Flugzeugkabine (4) nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass Stauräume unter dem erhöhten Gang (32) angeordnet sind.
  9. Flugzeugkabine (4) nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass in den Zonen, in denen sich die Kojen (14) über Sitzen (12, 42) befinden, die Decke der Brücke im Wesentlichen parallel zur Brücke (20) ist.
EP05791092.9A 2004-07-26 2005-07-18 Anordnung des oberen teils einer flugzeugkabine Active EP1778540B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0408239A FR2873349B1 (fr) 2004-07-26 2004-07-26 Amenagement de la partie superieure de la cabine d'un aeronef
US60652204P 2004-09-02 2004-09-02
PCT/FR2005/001824 WO2006021646A1 (fr) 2004-07-26 2005-07-18 Amenagement de la partie superieure de la cabine d’un aeronef

Publications (2)

Publication Number Publication Date
EP1778540A1 EP1778540A1 (de) 2007-05-02
EP1778540B1 true EP1778540B1 (de) 2015-11-04

Family

ID=35197920

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05791092.9A Active EP1778540B1 (de) 2004-07-26 2005-07-18 Anordnung des oberen teils einer flugzeugkabine

Country Status (6)

Country Link
US (1) US7290735B2 (de)
EP (1) EP1778540B1 (de)
BR (1) BRPI0513621B1 (de)
CA (1) CA2573971C (de)
RU (1) RU2385825C2 (de)
WO (1) WO2006021646A1 (de)

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Publication number Priority date Publication date Assignee Title
CN110271674A (zh) * 2019-06-12 2019-09-24 曲阜市铸造材料厂 一种可旋转飞机卧铺

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US8991756B2 (en) * 2009-12-14 2015-03-31 Be Intellectual Property, Inc. Small diameter pressure structure commercial aircraft crew rest
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US10909397B2 (en) 2014-06-13 2021-02-02 B/E Aerospace, Inc. Aircraft suite including main cabin compartment and lower lobe rest compartment
US10824889B2 (en) 2014-06-13 2020-11-03 Rockwell Collins, Inc. Passenger rest compartments for remote aircraft spaces
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FR3035072B1 (fr) * 2015-04-20 2020-09-18 Airbus Operations Sas Aeronef a architecture d'espace sous-cabine amelioree
DE102015116804A1 (de) * 2015-10-02 2017-04-06 Airbus Operations Gmbh Raumeffizientes Kabinensegment für ein Fahrzeug sowie eine Passagierkabine mit einer Mehrzahl von Sitzen und einem solchen Kabinensegment
US10597161B2 (en) * 2016-02-17 2020-03-24 B/E Aerospace, Inc. Space-optimizing seating arrangements for passenger transport and methods therefor
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CN110271674A (zh) * 2019-06-12 2019-09-24 曲阜市铸造材料厂 一种可旋转飞机卧铺
CN110271674B (zh) * 2019-06-12 2021-10-12 曲阜市铸造材料厂 一种可旋转飞机卧铺

Also Published As

Publication number Publication date
BRPI0513621A (pt) 2008-05-13
EP1778540A1 (de) 2007-05-02
WO2006021646A1 (fr) 2006-03-02
BRPI0513621B1 (pt) 2017-11-07
RU2007106892A (ru) 2008-09-10
CA2573971A1 (en) 2006-03-02
US20060113427A1 (en) 2006-06-01
RU2385825C2 (ru) 2010-04-10
US7290735B2 (en) 2007-11-06
CA2573971C (en) 2013-07-02

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